SID97-3A FAA APPROVED SUPERSEDES M73-22, M89-10 & M92-17
|
|
- Emery Shaw
- 7 years ago
- Views:
Transcription
1 TELEDYNE CONTINENTAL AIRCRAFT ENGINE SERVICE INFORMATION DIRECTIVE Compliance Will Enhance Safety, Maintenance or Economy Of Operation CATEGORY 4 SID97-3A FAA APPROVED SUPERSEDES M73-22, M89-10 & M92-17 SUBJECT: PURPOSE: COMPLIANCE: MODELS AFFECTED: PROCEDURES AND SPECIFICATIONS FOR ADJUSTMENT OF TELEDYNE CONTINENTAL MOTORS (TCM) CONTINUOUS FLOW FUEL INJECTION SYSTEMS. Provide procedures and specifications for the adjustment of Teledyne Continental Motors (TCM) fuel injection systems. At Engine Installation, 100 hour/annual Inspection, fuel system component replacement or as required if operation is not within specifications. All TCM continuous flow fuel injected engine models except L/TSIO-360-RB, TSIO-520-L, LB, WB, GTSIO-520-F, K, N and GIO-550-A engine models. WARNING THE PROCEDURES AND VALUES PROVIDED IN THIS SERVICE BULLETIN APPLY TO TCM FUEL INJECTED ENGINES THAT HAVE NOT BEEN MODIFIED FROM THEIR ORIGINAL TYPE DESIGN. REFER TO SUPPLEMENTAL TYPE CERTIFICATE (STC) HOLDER INFORMATION AND INSTRUCTIONS FOR AIRCRAFT AND ENGINES THAT HAVE BEEN MODIFIED FROM THEIR ORIGINAL TYPE DESIGN. GENERAL INFORMATION Fuel injection system components manufactured by TCM are adjusted and calibrated to meet engineering specifications. This insures operation within those specifications throughout the full range of operation. Fuel injection system components installed on factory new and rebuilt engines are further adjusted to meet design specifications during operation in the production engine test facility. These tests and adjustments are carried out in an environment of controlled fuel supply pressures and calibrated test equipment. When engines are installed in aircraft, they are subjected to a different induction system, fuel supply system and operating environment. These differences require checking and adjusting the fuel injection system to meet operational specifications before flight. Aircraft and engines that have been modified from their original type design must have the fuel injection system maintained in accordance with the Supplemental Type Certificate Holder s FAA approved instructions. Operational verification of the engine fuel system is required any time one of the following circumstances occurs: (1) at engine installation, (2) during 100 hour and annual inspections, (3) whenever a fuel system component is replaced or adjusted, (4) when changes occur in the operating environment. CAUTION... Engine performance, service life and reliability will be compromised if the engine's fuel injection system is neglected. The following adjustment procedures are presented in a sequential format that must be followed to insure proper fuel system adjustment. Reference the applicable Aircraft Maintenance Manual for detailed fuel system adjustment and maintenance procedures. MO DAY YEAR MO DAY YEAR 1 of TELEDYNE TECHNOLOGIES, INC.
2 Any fuel system that cannot be adjusted to meet the specified values will require repair or replacement of the affected components prior to further engine operation. The adjustment procedures provided in this SID also apply to engine fuel systems equipped with TCM Position Tuned Fuel Nozzles. Refer to Form X306474, Position Tuned Fuel Nozzle Installation and Maintenance Manual for more detailed information and installation instructions. CAUTION... Refer to the torque specifications, Table 1, page 9 for specified values when torquing hose end fittings. A. ADJUSTMENT TOOLS AND EQUIPMENT REQUIRED A complete set of tools and test equipment is essential for correct setup of TCM fuel injection systems. Various combinations of these tools and equipment will be used, depending on the engine model. A proper inventory of tools and equipment for fuel system adjustment will include the following: 1. TCM recommends the Model 20 ATM-C Porta Test Unit P/N ATM-C or equivalent to insure the fuel injection system meets all pressure and flow specifications. You may acquire a Model 20 ATM-C Porta Test Unit by contacting the following company: AERO TEST, Inc Goddard Road Romulus, Michigan (734) An alternative procedure would be to use calibrated gauges. 1. One (1) calibrated 0-60 PSI gauge, graduated in 1 PSI increments. This gauge will be used for unmetered pressure measurement. 2. One (1) calibrated 0-30 PSI gauge, graduated in.2 PSI (maximum) increments. This gauge will be used for metered pressure measurements and verification of aircraft fuel flow gauge indications on normally aspirated engines only. 3. One (1) calibrated differential gauge, 0-30 PSID maximum, graduated in.2 PSI (maximum) increments. This gauge will be used for metered pressure measurements and verification of aircraft fuel flow gauge on turbocharged engines only. NOTE Pressure gauges must be accurate within ±1 %. Pressure gauges must be checked for accuracy and, if necessary, calibrated at least once each calendar year. Calibrated pressure gauges may be purchased from various suppliers such as: Davis Instruments 4701 Mount Hope Drive Baltimore, MD Phone: or Two (2) P/N MS51523-B4 swivel tee. These fittings will be used to tee into fuel lines for unmetered and metered pressure reference. 5. Hoses of appropriate diameters and sufficient lengths to allow personnel and equipment to be located away from propeller arc and blast area. 6. Common hand tools including: 7/8, 11/16, 9/16, 1/2, 3/8, 7/16, 11/32, and 5/16 wrenches. A 1/4 drive ratchet and sockets, universal swivel, extension, and a 5/32 allen wrench common screw driver, a calibrated torque wrench, an oil can, mirror and flashlight. Safety equipment including hearing and eye protection must be used. 7. Tachometer verification instrument - various types are available. Verify aircraft tachometer accuracy prior to fuel system adjustment. B. PRE-SETUP PROCEDURES 1. During engine installation, or if any fuel system component has been replaced, flush the aircraft fuel system by first removing the engine-driven fuel pump inlet hose and terminating the end into a large, clean container. Operate the aircraft boost pump and allow a minimum of one gallon of fuel to flow through the system. Take necessary precautions to prevent a fire hazard. If contamination is present, locate and correct the source, and repeat this step before proceeding. MO DAY YEAR MO DAY YEAR 2 of 32
3 2. Before making any checks or adjustments, verify the accuracy of the aircraft tachometer, manifold pressure gauge and fuel flow gauge. Any gauge found to be inaccurate must be repaired or replaced before adjusting the fuel system. WARNING USE OF INACCURATE GAUGES WILL RESULT IN INCORRECT ADJUSTMENT OF THE ENGINE FUEL SYSTEM, POSSIBLE CYLINDER WEAR DUE TO LEAN OPERATION, PRE-IGNITION, DETONATION, LOSS OF POWER AND SEVERE ENGINE DAMAGE. 10. Inspect the throttle and control assembly link rods (where used) for correct installation, security and wear at the attach points. Correct any discrepancies noted. 11. Insure all engine controls operate freely throughout their full range of travel and are properly adjusted in accordance with the aircraft manufacturer's instructions. 12. Lubricate all control rod ends and fuel system components in accordance with the latest revision of TCM Service Bulletin SB95-2 and the Aircraft Maintenance Manual. WARNING 3. Remove the engine cowling in accordance with the aircraft manufacturer's instructions. 4. Insure that all fuel system components are of the correct part number and are installed properly. Correct any discrepancies noted. 5. Remove, inspect, clean and reinstall the aircraft and engine fuel screens in accordance with the aircraft manufacturer's instructions. 6. Inspect the aircraft induction air filter and alternate air system for condition, operation and cleanliness. Repair or replace any component that is not airworthy in accordance with the aircraft manufacturer's instructions. 7. Inspect the aircraft vapor return system for proper operation in accordance with the aircraft manufacturer s instructions. Correct any discrepancies noted. 8. Insure the fuel manifold valve vent and fuel pump drain lines are properly installed, open and free of obstruction. Correct any discrepancies noted. 9. Inspect all engine control rod ends for wear, freedom of movement, proper installation and security in accordance with the aircraft manufacturer's instructions. Correct any discrepancies noted. FAILURE TO CORRECTLY INSTALL AND MAINTAIN ENGINE CONTROLS CAN RESULT IN LOSS OF SYSTEM CONTROL AND SUBSEQUENT LOSS OF ENGINE POWER. 13. Locate the IDLE speed stop screw on the throttle body and turn it counter-clockwise two complete turns. See Figures 6, through 9. During fuel system adjustment, IDLE RPM will be controlled manually using the cockpit throttle control. 14. Inspect the exhaust and induction systems for proper installation, security and leaks. Correct any discrepancies noted. 15. Inspect all lines, hoses and wire bundles for chafing, loose connections, leaks and stains. Correct any discrepancies noted. Turbocharged engine models incorporating a fuel pressure regulator must have the regulator deactivated during initial fuel system adjustment. To deactivate the fuel pressure regulator, loosen and remove the fuel line or hose from the center port fitting at the pressure regulator. Refer to Figure 10. Install and torque, to the specified value, a cap on the center port fitting. Install and torque, to the value specified, a plug onto the removed line. Pressure test these areas for fuel leaks prior to proceeding with the fuel system adjustments. MO DAY YEAR MO DAY YEAR 3 of 32
4 C. SETUP PROCEDURES WARNING DURING REMOVAL AND INSTALLATION OF FUEL LINES AND HOSES, FAILURE TO PROPERLY SUPPORT COMPONENT FITTINGS CAN RESULT IN FITTING AND/OR COMPONENT DAMAGE AND LOSS OF SYSTEM. REFERENCE THE LATEST REVISION OF TCM SERVICE BULLETIN SIL95-5. NOTE... Adjustments to any component of the fuel injection system can affect other system settings. Always verify the performance of the entire fuel injection system whenever any fuel injection system component is adjusted. 1. Loosen and remove the unmetered fuel supply hose from either the fuel pump outlet fitting or the fuel control unit inlet fitting, whichever is most accessible. Some engine models have an unmetered fuel pressure connection you can access at the fuel control screen. 2. Install and torque the MS51523-B4 swivel tee directly to the fuel pump outlet fitting or to the fuel control inlet fitting as applicable. NOTE... Some installations may require combinations of different fittings and hoses to facilitate installation of unmetered and metered test equipment connections. 3. Attach the unmetered fuel supply hose to the straight end of the tee connector and torque. 4. Connect the Unmetered test hose from the Porta Test Unit to the tee fitting and torque. If using the alternative procedure, connect the 0-60 PSI gauge to the swivel tee using a length of hose which will provide proper clearance from the engine cowling and propeller arc. Torque all connections. 5. Loosen and remove the metered fuel supply hose from the manifold valve inlet fitting. 6. Install and torque the second MS51523-B4 swivel tee directly to the fuel manifold valve inlet fitting. 7. Attach the metered fuel supply hose to the straight end of the tee connector and torque. 8. Connect the metered pressure test hose from the Porta Test Unit to this second tee connector and torque. If using the alternative procedure, connect the 0-30 PSI gauge to the swivel tee using a hose long enough to provide proper clearance from the engine cowling and propeller arc. Torque all connections. 9. On turbocharged engines, connect the Porta- Test Manifold Pressure and Upper Deck Pressure hose to the engine following the instructions provided with the Porta Test Unit. If using the alternative procedure, connect the 0-30 PSId differential gauge pressure fitting to the metered pressure swivel tee using a hose of sufficient length to provide clearance from the aircraft and propeller arc. Connect an equal length of hose to the "suction" side of the gauge and connect the other end to a location to reference turbocharger compressor discharge (upper deck) pressure. See Figure 12. Torque all connections. 10. Position the throttle control in the FULL OPEN position and the mixture control to FULL RICH. Operate the aircraft boost pump in accordance with the aircraft manufacturer's instructions. Following the instructions provided with the Porta Test Unit, bleed all air from the test unit and hoses. If using the alternative calibrated test gauges, loosen the test connections at each gauge to bleed the lines of any air. Hold the gauge at or slightly above the height of the fuel system component during the bleeding operation. Operate the boost pump only long enough to allow purging of air from the installed test equipment. Verify that all fuel lines, hoses and fittings are secured and torqued and that no fuel leaks exist before proceeding. Insure test hoses have been routed clear of the exhaust system and are supported their entire length to avoid inaccurate gauge readings. MO DAY YEAR MO DAY YEAR 4 of 32
5 WARNING MAKE CERTAIN ALL FUEL HAS DRAINED FROM THE INDUCTION SYSTEM PRIOR TO ATTEMPTING ENGINE START. FAILURE TO DO SO COULD CAUSE HYDRAULIC LOCK AND SUBSEQUENT ENGINE FAILURE. 11. Install the engine cowling or cooling shroud during ground operation. 12. Refer to TABLE 3, beginning on page 11, for specific data applicable to your engine. Record the applicable IDLE and FULL POWER adjustment points: RPM, fuel pressure, fuel flows, manifold pressure and fuel/air mixture rise provided in this Service Bulletin and Aircraft Maintenance Manual on the operational test form included at the end of this service bulletin. The Operational Test Form may be reproduced for use in recording adjustments and test indications. NOTE... To insure optimum cooling during FULL POWER operations, the FULL POWER fuel flow should be set to the maximum specification limit. WARNING BEFORE STARTING THE ENGINE INSURE THAT THE AIRCRAFT WHEELS ARE CHOCKED AND BRAKES ARE SET. 13. Prepare the aircraft for ground run and start the engine in accordance with the aircraft manufacturer's instructions. Advance the throttle to 1500 to 1800 RPM. While monitoring all engine gauges, operate the engine at this speed until the engine temperatures and pressures have stabilized in the operational range. Use the operational test form to record the gauge indications. NOTE Test gauge readings must be taken with the gauges held at the same height above the ground as the fuel system component it is attached to. 14. With the mixture control in the FULL RICH position, reduce the throttle to the specified IDLE RPM. Record the unmetered pressure indicated on the gauge. Slowly move the mixture control toward the IDLE CUT-OFF position and record the maximum RPM rise. Return the mixture control to FULL RICH. 15. Monitoring all engine gauges, slowly advance the throttle control to full rated power for the engine and allow the engine to stabilize for 15 seconds. Record all engine and test gauge indications. DO NOT ALLOW ENGINE TEMPERATURES TO EXCEED 420 F CHT AND 210 F OIL TEMP. Retard throttle control to 800 to 1000 RPM. NOTE... L/TSIO-360 and TSIO-520 model engines with a fixed (ground adjustable) exhaust bypass, verify that the wastegate is adjusted in accordance with the aircraft manufacturer's instructions. Failure to do so can result in an improperly adjusted fuel system and possible engine damage. CAUTION... After FULL POWER operation - turbocharged engines must be operated at 800 to 1000 RPM for a minimum of five (5) minutes to allow engine temperatures to stabilize prior to engine shutdown. 16. Compare the recorded IDLE fuel pressure, IDLE RPM fuel/air mixture rise and full power RPM, manifold pressure (as applicable), unmetered fuel pressure, metered fuel pressure and fuel flow indications with the specified values. If all recorded values are within specifications, proceed to paragraph 24. NOTE... Turbocharged engines equipped with fuel pressure regulators should indicate a full power metered pressure and fuel flow five (5) percent higher than specified. This is required to insure adequate partthrottle fuel flow. 17. If any of the recorded readings are not within specifications, the fuel system must be completely adjusted. ALL READINGS MUST BE TAKEN WITH MIXTURE CONTROL IN THE FULL RICH POSITION. MO DAY YEAR MO DAY YEAR 5 of 32
6 Install the engine cowling or cooling shroud during all ground operation. NOTE... Engine driven fuel pump output pressures vary with engine RPM. During ground operation FULL POWER RPM may not be obtained. Use the Fuel Flow Compensation Table 2 on page 10 to correct the specified metered pressures if FULL POWER RPM cannot be achieved. On turbocharged engines insure that the manifold pressure is adjusted in accordance with the aircraft manufacturer s instructions. Engine driven fuel pumps installed on turbocharged engines are referenced to turbocharger compressor discharge pressure (upper deck pressure) to achieve FULL POWER engine driven fuel pump pressure. WARNING MAKE ALL ADJUSTMENTS WITH THE ENGINE STOPPED AND THE IGNITION AND MASTER SWITCHES IN THE OFF POSITION. 18. To adjust the IDLE RPM unmetered pump pressure, loosen the lock nut on the low pressure relief valve. See Figures 1 through 5. Turning the adjustment clockwise (CW) will increase pressure and counterclockwise (CCW) will decrease pressure. Operate the engine at RPM for 15 seconds after each adjustment, then retard the throttle to the specified IDLE RPM. Repeat this step until pressure is within specified limits. NOTE... Maximum part throttle full rich fuel flow will be achieved by setting the idle rpm (low) unmetered fuel pump pressure to the minimum value specified. With the idle rpm fuel/air mixture properly adjusted (step 19) the fuel control metering plate orifices are indexed to the maximum open position. 19. With engine operating at the specified IDLE RPM and unmetered fuel pressure, slowly move the mixture control from the FULL RICH position toward IDLE CUT-OFF to check fuel/air mixture. A rise of 25 to 50 RPM should be obtained. An RPM change greater than 50 indicates the mixture is too rich and a change that is less than 25 indicates the mixture is too lean. Adjust mixture conditions that are too rich or too lean as follows: a) Identify the type of throttle and control assembly that is to be adjusted. See Figures 6, 8 and 9. b) Perform an IDLE fuel/air mixture check and observe RPM rise. If the RPM rise is not within specifications, advance the throttle control to RPM for 15 seconds after each adjustment to clear the engine. Retard the throttle control to IDLE RPM and repeat mixture check. Make the necessary adjustment. Repeat this procedure until the specified RPM rise is achieved. c) Recheck IDLE RPM unmetered pump pressure. If pressure in not within limits, repeat Steps 18, 19, 19-a and 19-b before continuing. 20. On all naturally aspirated engines, adjust the FULL POWER metered fuel pressure to the specified value by turning the adjustable orifice screw clockwise to increase fuel pressure and counterclockwise to decrease fuel pressure. See Figures 1, 2 and On turbocharged engines, adjust the full power metered fuel pressure to the specified value as follows: NOTE... On turbocharged engines equipped with a fuel pressure regulator, the full power metered fuel pressure and fuel flow must be adjusted to five (5) percent higher than the maximum specified limit. a. Loosen the aneroid adjustment screw lock nut. See Figures 4 and 5. b. Turn the aneroid adjustment screw counterclockwise to increase metered fuel MO DAY YEAR MO DAY YEAR 6 of 32
7 pressure and clockwise to decrease metered fuel pressure. c. After final adjustment is accomplished, torque lock nut to inch pounds. DO NOT EXCEED LOCK NUT TORQUE LIMITS. OVER-TORQUING OF LOCK NUT WILL RESULT IN DAMAGE TO ANEROID HOUSING THREADS AND SUBSEQUENT LOSS OF ADJUSTMENT. 22. For engines equipped with a fuel pressure regulator, the full power metered fuel pressure and fuel flow must now be set to the specified limit by adjustment of the regulator as follows. See Figure 10. Reconnect the regulator and torque all connections to the specified value. Loosen the lock nut on the regulator adjustment. Turn the regulator adjusting screw clockwise to increase metered fuel pressure and fuel flow and counterclockwise to decrease metered fuel pressure and fuel flow. After final adjustment is completed, torque the lock nut to the specified value. 23. When full power metered fuel pressure has been adjusted to the specified values, recheck: (a) IDLE RPM, (b) unmetered fuel pressure, (c) fuel/air mixture. If any values are not within specified limits, repeat the adjustment procedures. 24. With the fuel system set to the specified metered fuel pressure, set the IDLE RPM to the aircraft manufacturer s specified value by turning the Idle Speed Stop screw clockwise to increase RPM or counterclockwise to decrease RPM. See Figures 6, 8 and 9. D. POST SETUP PROCEDURES 1. Insure that the master switch, ignition switch and fuel selector are in the OFF position. 2. Remove the engine cowling or cooling shroud in accordance with the aircraft manufacturer's instructions. (a) remove all test gauges, fittings and hoses that were installed for fuel system setup, (b) reconnect all fuel hoses to their original locations, (c) support and torque all fittings to the specified value, see TABLE Perform a complete fuel system leak check in accordance with the aircraft manufacturer's instructions. Correct any discrepancies noted. 4. Install engine cowling in accordance with the aircraft manufacturer's instructions. 5. Perform a complete operational ground run-up and verify that all fuel system performance specifications are achieved. E. FLIGHT TEST: Except naturally aspirated engines with altitude compensating fuel pump 1. Refer to the aircraft manufacturer s or Supplemental Type Certificate (STC) holder s POH/AFM for specific operational information. 2. A flight test is required whenever an adjustment is made that may affect engine operational characteristics or performance. 3. If FULL POWER RPM was not obtained during fuel injection system setup and adjustment, a flight test is required to insure that the fuel injection system is performing within specified limits for the engine and aircraft. 4. Repeat the setup and adjustments as required until the fuel injection system is performing within the published specification for the aircraft and engine. F. FLIGHT TEST: Naturally Aspirated engines with altitude compensating fuel pumps (AUTO LEAN) 1. All naturally aspirated engines utilizing an altitude compensating fuel pump require a flight test every 100 hours or annual inspection and anytime an adjustment is made to the fuel injection system to insure proper operation of the fuel pump auto leaning feature. MO DAY YEAR MO DAY YEAR 7 of 32
8 2. TABLE 4 and Auto Leaning Chart 1 provides fuel flow vs. pressure altitude specifications for the IO-360-DB engine with altitude compensating fuel pump. Tables 6 & 7 and Auto Leaning Charts 2 & 3 provide fuel flow vs. pressure altitude specifications for the IO- 360-ES engine with altitude compensating fuel pump. Tables 8 through 11 and Auto Leaning Charts 4 through 7 provide fuel flow vs. pressure altitude specifications for the IO-550- series engine with altitude compensating fuel pump. 3. Insure the accuracy of aircraft fuel flow gauge and tachometer has been verified. These gauges must be accurate or the data recorded during flight test will not be valid. 4. Locate the correct table and auto leaning chart for the aircraft and engine. On the operational test form provided in this Service Information Directive, record all pressure altitudes and corresponding minimum and maximum fuel flows as specified. 5. In accordance with the aircraft manufacturer s instructions, perform a complete preflight inspection, engine start and ground runup. 6. Set the aircraft altimeter to inches Hg. 7. In accordance with the aircraft manufacturer s instructions, conduct a normal take-off. 8. Climb must be accomplished using full throttle, FULL RICH mixture and maximum rated full power RPM. 9. Using the aircraft fuel flow gauge and altimeter, record fuel flows at all pressure altitudes specified. 10. Compare the recorded fuel flows with the specified fuel flows for all pressure altitudes. If fuel flows are within the minimum and maximum limits at all altitudes, no adjustments are required. 11. If the fuel flows are not within specified limits at all pressure altitudes, the fuel injection system auto leaning schedule requires adjustment. G. ADJUSTMENT PROCEDURES: Fuel Pump Auto Leaning Schedule NOTE... On IO-550-A and C model engines do not attempt to adjust the auto leaning schedule if the aircraft is at a field with a pressure altitude greater than 1000 feet. On IO-550-B, D, E, F and L model engines, do not attempt to adjust the auto leaning schedule if the aircraft is at a field with a pressure altitude greater than 3000 feet. Refer to Part C of this Service Information Directive for installation of the required test equipment. 1. If not previously accomplished, adjust the engine fuel injection system in accordance with Part C of this Service Information Directive using the appropriate table for the engine and aircraft. 2. Adjustments to the engine-driven fuel pump variable orifice (aneroid) will result in a change to the auto leaning schedule. One complete revolution of the aneroid adjustment will increase or decrease the auto leaning schedule approximately 1000 feet. 3. Refer to the charts on pages 19 to 25. The variable orifice (aneroid) adjustment will move you horizontally across the chart. The adjustable orifice will move you vertically. 4. Adjustments to the variable orifice (aneroid) will affect the FULL POWER unmetered fuel pressures (adjustable orifice), metered pressures and fuel flows. It is important to maintain the balance between these adjustments in order to achieve the specified fuel system parameters. CAUTION Exercise caution when adjustments to the aneroid are accomplished. The aneroid stem has an extra fine thread and over-torqueing the lock nut will damage either the stem or housing threads. MO DAY YEAR MO DAY YEAR 8 of 32
9 NOTE... It will be necessary to cut and remove the safety wire and manufacturer s seal from the variable orifice adjustment. Cut the safety wire as close to the variable orifice stem as possible. This will provide a pigtail for the fuel pump through bolts. It is not necessary to resafety the aneroid after adjustments have been completed. 5. By reviewing the data recorded on the operational test flight form, we can determine if the auto leaning schedule is above or below the specified limits at the various pressure altitudes. 6. Adjustment of the variable orifice (aneroid) clockwise will decrease the altitude (move horizontally to the left on the chart) while counterclockwise adjustments will increase the altitude (move horizontally to the right on the chart) at a given pressure altitude. 7. As an example, looking at chart number 5 (IO- 550-B engine) at a pressure altitude of 4000 feet the recorded fuel flow was 140 PPH (point A). The fuel flow specified for this pressure altitude is 142 PPH to 152 PPH. The recorded fuel flow of 140 PPH would be correct if we were between 5000 feet and 7000 feet. To achieve the specified fuel flow versus pressure altitude we must adjust the variable orifice out. Adjustment of the variable orifice (aneroid) two complete revolutions will move point A two thousand feet to the right to 6000 feet. 8. After making any adjustment to the variable orifice, torque the lock nut to inch pounds. 9. Perform a complete ground run-up and verify that unmetered and metered pressures and fuel flows are within the limits specified in the appropriate table for the pressure altitude. If these parameters are not within the limits specified make adjustments in accordance with PART C to achieve the specified values. NOTE... The adjustable orifice tapered needle may be damaged if forced against its seat. The adjustment should move freely. Do not continue adjustments if rotational resistance increases suddenly. 10. Once the adjustments are completed, remove the test equipment in accordance with part D (Post Setup Procedures). 11. Perform a flight test in accordance with part F (Flight Test: Naturally Aspirated engines with Auto Lean). 12. Repeat these procedures until the engine s fuel injection system meets all published specifications. MO DAY YEAR MO DAY YEAR 9 of 32
10 TABLE 1 Torque Specifications for Hose End Fittings BRASS or ALUMINUM END FITTINGS STEEL HOSE END FITTINGS Hose Size Fitting Material Torque (inch lbs.) Hose Size Fitting Material Torque (inch lbs.) #2 (.31x24) Hose end fitting #2 (.31x24) Steel End Fitting Brass/Aluminum #3 Hose end fitting #3 Steel End Fitting (.38x24) Brass/Aluminum (.38x24) #4 Hose end fitting #4 Steel End Fitting (.4375x20) Brass/Aluminum (.4375x20) #5 Hose end fitting #5 Steel End Fitting (.500x20) Brass/Aluminum (.500x20) #6 Hose end fitting #6 Steel End Fitting (.5625x18) Brass/Aluminum (.5625x18) #8 Hose end fitting #8 Steel End Fitting (.750x16) Brass/Aluminum (.750x16) #10 Hose end fitting #10 Steel End Fitting (.875x14) Brass/Aluminum (.875x14) #12 (1.063x12) Hose end fitting Brass/Aluminum #12 (1.063x12) Steel End Fitting Table 2. Compensation Table For Static Ground Setup Metered Pressure vs. 70 F Fuel Temperature Static Engine RPM Correction Factor Corrected Metered Pressure (Metered Pressure x Correction Factor) Rated RPM NOTE: All values are approximate. Variations may occur due to engine and installation specific influences. Example: IO-520-BB, Maximum Rated RPM = Metered Fuel Pressure Limits = If maximum static engine RPM = 2640, (-60 RPM) use Correction Factor.973 Metered Fuel Pressure Limits x Correction Factor = Corrected Metered Pressure Limits 14.9 x.973 = 14.5 (Minimum Metered Pressure 2640 RPM 17.2 x.973 = 16.7 (Maximum Metered Pressure 2640 RPM MO DAY YEAR MO DAY YEAR 10 of 32
11 ENGINE TABLE 3. Fuel System Adjustment Values IDLE AND FULL POWER FUEL S AND FLOWS Prop. RPM & (MAP) Unmetered Pump PSI (NOTE 3) Metered Nozzle PSI (NOTE 4) Fuel lbs/hr Fuel gal/hr (NOTE 5) (NOTE6) IO-240-A, B See latest revision of TCM SID for fuel system values for IO-240-B3Band B9B engines IO-346-A, B IO-360-A, AB, C CB, D, DB, G, GB, H, HB, J, JB IO-360-ES SEE NOTE IO-360-ES (6) SEE NOTE 2& Sea Level IO-360-ES (6) SEE NOTE 2& ,500 Press Alt Engines with Altitude Compensating fuel pumps See Note 2 page 18 of 31. IO-360-K, KB TSIO-360-A, AB (32.0) TSIO-360-B, BB (32.0) TSIO-360-C, CB (37.0) MO DAY YEAR MO DAY YEAR 11 of 32
12 ENGINE TABLE 3. Fuel System Adjustment Values (cont d) IDLE AND FULL POWER FUEL S AND FLOWS Prop. RPM & (MAP) Unmetered Pump PSI (NOTE 3) Metered Nozzle PSI (NOTE 4) Fuel lbs/hr Fuel gal/hr (NOTE 5) (NOTE 6) TSIO-360-D, DB (36.0) TSIO-360-E, EB, L/TSIO-360-E, EB (40.0) TSIO-360-F, FB (41.0) TSIO-360-G, GB (40.0) TSIO-360-H, HB (34.5) TSIO-360-JB (37.0) TSIO-360-KB, L/TSIO-360-KB (40.0) TSIO-360-LB (40.0) TSIO-360-MB (36.0) MO DAY YEAR MO DAY YEAR 12 of 32
13 ENGINE TABLE 3. Fuel System Adjustment Values (cont d) IDLE AND FULL POWER FUEL S AND FLOWS Prop. RPM & (MAP) Unmetered Pump PSI (NOTE 3) Metered Nozzle PSI (NOTE 4) Fuel lbs/hr Fuel gal/hr (NOTE 5) (NOTE 6) L/TSIO-360-RB Minimum SEE NOTE (38.0) TSIO-360-SB (39.0) O-470-GCI IO-470-C, G, P, R IO-470-D, E, F, H L, M, N, S, U IO-470-J, K IO-470-V IO-470-VO GIO-470-A TSIO-470-B, C, D (35.0) IO-520-A, J IO-520-B, BA, BB C, CB MO DAY YEAR MO DAY YEAR 13 of 32
14 ENGINE TABLE 3. Fuel System Adjustment Values (cont d) IDLE AND FULL POWER FUEL S AND FLOWS Prop. RPM & (MAP) Unmetered Pump PSI (NOTE 3) Metered Nozzle PSI (NOTE 4) Fuel lbs/hr Fuel gal/hr (NOTE 5) (NOTE 6) IO-520-D, F, K, L IO-520-E IO-520-M, MB IO-520-P LIO-520-P TSIO-520-AE, L/TSIO-520-AE (32.5) TSIO-520-AF (35.5) TSIO-520-B, BB (32.0) TSIO-520-BE (38.0) TSIO-520-C, H (32.5) TSIO-520-CE (37.0) MO DAY YEAR MO DAY YEAR 14 of 32
15 ENGINE TABLE 3. Fuel System Adjustment Values (cont d) IDLE AND FULL POWER FUEL S AND FLOWS Prop. RPM & (MAP) Unmetered Pump PSI (NOTE 3) Metered Nozzle PSI (NOTE 4) Fuel lbs/hr Fuel gal/hr (NOTE 5) (NOTE 6) TSIO-520-D, DB (32.5) TSIO-520-E, EB (34.5) TSIO-520-G (35.0) TSIO-520-J, JB (36.0) TSIO-520-K, KB (33.0) TSIO-520-L, LB Minimum SEE NOTE 1 (38.0) TSIO-520-M, R (36.5) TSIO-520-N, NB (38.0) TSIO-520-P (36.5) MO DAY YEAR MO DAY YEAR 15 of 32
16 ENGINE TABLE 3. Fuel System Adjustment Values (cont d) IDLE AND FULL POWER FUEL S AND FLOWS Prop. RPM & (MAP) Unmetered Pump PSI (NOTE 3) Metered Nozzle PSI (NOTE 4) Fuel lbs/hr Fuel gal/hr (NOTE 5) (NOTE 6) TSIO-520-T (39.5) TSIO-520-UB (36.0) TSIO-520-VB (40.5) TSIO-520-WB Minimum SEE NOTE 1 (39.5) GTSIO-520-C (34.5) GTSIO-520-D, H (39.5) GTSIO-520-F, K SEE NOTE (44.5) GTSIO-520-L (39.0) GTSIO-520-M (40.0) GTSIO-520-N SEE NOTE (39.0) MO DAY YEAR MO DAY YEAR 16 of 32
17 ENGINE TABLE 3. Fuel System Adjustment Values (cont d) IDLE AND FULL POWER FUEL S AND FLOWS Prop. RPM & (MAP) Unmetered Pump PSI (NOTE 3) Metered Nozzle PSI (NOTE 4) Fuel lbs/hr Fuel gal/hr (NOTE 5) (NOTE 6) IO-550-A Engines with Altitude Compensating fuel pumps See Note 2 page 18 of 31. IO-550-B SEE NOTE Engines with Altitude Compensating fuel pumps See Note 2 page 18 of 31. IO-550-C SEE NOTE Engines with Altitude Compensating fuel pumps See Note 2 page 18 of 31. IO-550-D, E, F, L SEE NOTE Engines with Altitude Compensating fuel pumps See Note 2 page 18 of 31. IO-550-G IO-550-N IO-550-P IO-550-R GIO-550-A Minimum See NOTE TSIO-550-B (38.0) TSIO-550-C (35.5) MO DAY YEAR MO DAY YEAR 17 of 32
18 ENGINE TABLE 3. Fuel System Adjustment Values (cont d) IDLE AND FULL POWER FUEL S AND FLOWS Prop. RPM & (MAP) Unmetered Pump PSI (NOTE 3) Metered Nozzle PSI (NOTE 4) Fuel lbs/hr Fuel gal/hr (NOTE 5) (NOTE 6) TSIO-550-E (38.5) TSIOL-550-A (38.0) TSIOL-550-B (35.0) TSIOL-550-C (39.5) (TIARA) See latest revision of Teledyne Continental Motors Service Bulletin M79-4. NOTE 1: NOTE 2: NOTE 3: NOTE 4: NOTE 5: NOTE 6: Refer to the aircraft manufacturer s instructions for adjustment procedures. Flight test required to verify fuel flow vs. pressure altitude values are within the limits specified. See applicable Tables 4 through 10 and Charts 1 through 7 for specified values. FULL POWER unmetered fuel pump pressure limits are provided for reference only. Use metered fuel pressure specifications for adjustments at full power. Use for full power, maximum RPM adjustment only. All other parameters for reference only, see note above. May be determined using a calibrated in-line flow measuring device. Otherwise use metered fuel pressure specifications. Refer to Aircraft Manufacturer s Maintenance Manual for method of verifying accuracy of fuel flow indicator. This engine installed in Cirrus SR20 aircraft. IO-360-ES (6) B engine has been derated by Cirrus from original 210 HP at 2800 RPM to 200 HP at RPM. Engine data plate reflects original TC and PC data of 210 HP at 2800 RPM. Refer to Cirrus SR20 Maintenance Manual and Pilots Operating Handbook. MO DAY YEAR MO DAY YEAR 18 of 32
19 TABLE 4. ALTITUDE FUEL SCHEDULE IO-360-DB ENGINE FULL OPEN THROTTLE, FULL RICH MIXTURE 2800 RPM Pressure Altitude (Set Altimeter at (lbs/hr) (gals/hr) Metered Fuel Pressure PSID in. Hg.) Min. Max. Min. Max. Min. Max. Sea Level , , , , , , , , , , , Gasoline = 5.87 lbs per 70 F. IO-360-DB Installed in T-41 ACFT Refer to Cessna SL 81-2 date 28 July 1981 for amplified instructions. Altitude Leaning Schedule IO-360-DB-(34) Altitude (X 1000 ft) CHART 1 MO DAY YEAR MO DAY YEAR 19 of 32
20 TABLE 5. ALTITUDE FUEL SCHEDULE IO-360 ES ENGINE FULL OPEN THROTTLE, FULL RICH MIXTURE 2800 RPM Pressure Altitude (Set Altimeter at (lbs/hr) (gals/hr) Metered Fuel Pressure PSID in. Hg.) Min. Max. Min. Max. Min. Max. Sea Level , , , , , , , , , , , Gasoline = 5.87 lbs per 70 F. 110 ALTITUDE LEANING SCHEDULE IO-360-ES 2800 R.P.M. and FULL RICH MIXTURE FULL OPEN THROTTLE Fuel- 100/100LL Full Rich, 2800 PRM Fuel Temp 72 F 95 (pph) Altitude (X 1000 ft) CHART 2 MO DAY YEAR MO DAY YEAR 20 of 32
21 TABLE 6. ALTITUDE FUEL SCHEDULE IO-360 ES ENGINE FULL OPEN THROTTLE, FULL RICH MIXTURE RPM Pressure Altitude (Set Altimeter at (lbs/hr) (gals/hr) Metered Fuel Pressure PSID in. Hg.) Min. Max. Min. Max. Min. Max. Sea Level , , , , , , , , , , , Gasoline = 5.87 lbs. per 70 F. 105 ALTITUDE LEANING SCHEDULE IO-360-ES (6) AT RPM FULL RICH MIXTURE & FULL OPEN THROTTLE Recommended Setup for Cirrus SR20 Installation WOT Fuel- 100/100LL Full Rich, RPM Fuel Temp 72 F 90 (PPH) Altitude (X 1000 ft) CHART 3 MO DAY YEAR MO DAY YEAR 21 of 32
22 Pressure Altitude (Set Altimeter at in. Hg.) TABLE 7. ALTITUDE FUEL SCHEDULE IO-550-A ENGINE FULL OPEN THROTTLE, FULL RICH MIXTURE 300 RPM (lbs/hr) Min. Max. (gals/hr) Min. Max. Metered Fuel Pressure PSID Min. Max. Sea Level , , , , , , , Gasoline = 5.87 lbs per 70 F 160 Altitude Leaning Schedule IO-550-A Full Rich, RPM Pressure Altitude (X 1000 ft) CHART 4 MO DAY YEAR MO DAY YEAR 22 of 32
23 TABLE 8. ALTITUDE FUEL SCHEDULE IO-550-B ENGINE FULL OPEN THROTTLE, FULL RICH MIXTURE 300 RPM Pressure Altitude (Set Altimeter at in. Hg.) (lbs/hr) (gals/hr) Metered Fuel Pressure PSID Sea Level Min. 146 Max. 156 Min Max Min , , , , , , , Gasoline = 5.87 lbs per 70 F. Max Altitude Leaning Schedule IO-550-B Full Rich, RPM Point A Aneroid adjusted out two turns Point A Pressure Altitude (X 1000 ft) CHART 5 MO DAY YEAR MO DAY YEAR 23 of 32
24 TABLE 9. ALTITUDE FUEL SCHEDULE IO-550-C ENGINE FULL OPEN THROTTLE, FULL RICH MIXTURE 300 RPM Pressure Altitude (Set Altimeter at in. Hg.) (lbs/hr) (gals/hr) Metered Fuel Pressure PSID Sea Level Min. 152 Max. 160 Min Max Min Max , , , , , , , Gasoline = 5.87 lbs per 70 F. 170 Altitude Leaning Schedule IO-550-C Full Rich, RPM Pressure Altitude (X 1000 ft) CHART 6 MO DAY YEAR MO DAY YEAR 24 of 32
25 Pressure Altitude (Set Altimeter at in. Hg.) TABLE 10. ALTITUDE FUEL SCHEDULE IO-550-D,-E, F, L ENGINE FULL OPEN THROTTLE, FULL RICH MIXTURE 300 RPM (lbs/hr) (gals/hr) Metered Fuel Pressure PSID Sea Level Min. 143 Max. 155 Min Max Min Max , , , , , , , Gasoline = 5.87 lbs per 70 F. 160 Altitude Leaning Schedule IO-550-D, -E, -F, -L Full Rich, RPM 150 ( ) Pressure Altitude (X 1000 ft) CHART 7 MO DAY YEAR MO DAY YEAR 25 of 32
26 VAPOR RETURN ADJUSTABLE ORIFICE CW = INCREASE FUEL INLET FUEL INLET FUEL RETURN DRAIN FUEL OUTLET (UNMETERED ) LOW RELIEF VALVE CW = INCREASE FUEL OUTLET (UNMETERED ) LOW RELIEF VALVE CW = INCREASE FIGURE 1 - NATURALLY ASPIRATED ENGINE FUEL PUMP ADJUSTABLE ORIFICE CW = INCREASE VAPOR RETURN FUEL INLET VAPOR RETURN (LOCATED ON OPPOSITE SIDE ON MOST FUEL PUMPS) FUEL INLET LOW RELIEF VALVE CW = INCREASE LOW RELIEF VALVE CW = INCREASE DRAIN FUEL OUTLET (UNMETERED ) IDLE CUTOFF FULL RICH FIGURE 2 - NATURALLY ASPIRATED ENGINE (MIXTURE CONTROL EQUIPPED) FUEL PUMP MO DAY YEAR MO DAY YEAR 26 of 32
27 VAPOR RETURN VAPOR RETURN ADJUSTABLE ORIFICE CW = INCREASE FUEL INLET FUEL INLET LOW RELIEF VALVE CW = INCREASE DRAIN AMBIENT REFERENCE FUEL OUTLET (UNMETERED ) ANEROID ADJUSTMENT FACTORY SET ADJUSTMENT NOT NORMALLY REQUIRED FIGURE 3 - ALTITUDE COMPENSATING FUEL PUMP FUEL INLET ANEROID ADJUSTMENT CCW = INCREASE FUEL INLET VAPOR RETURN FUEL RETURN TURBOCHARGE DISCHARGE REFERENCE DRAIN FUEL OUTLET (UNMETERED ) LOW RELIEF VALVE CW = INCREASE FIGURE 4 - ANEROID EQUIPPED FUEL PUMP TURBOCHARGED ENGINE MO DAY YEAR MO DAY YEAR 27 of 32
28 FUEL INLET VAPOR RETURN TURBOCHARGE DISCHARGE REFERENCE VAPOR RETURN ANEROID ADJUSTMENT CCW = INCREASE IDLE CUTOFF FULL RICH LOW RELIEF VALVE CW = INCREASE DRAIN FUEL OUTLET (UNMETERED ) FIGURE 5 - ANEROID & MIXTURE CONTROL EQUIPPED FUEL PUMP TURBOCHARGED ENGINE IDLE MIXTURE ADJUSTMENT CW = LEAN CCW = ENRICH IDLE SPEED STOP SCREW CW = INCREASE CCW = DECREASE FUEL OUTLET (METERED ) FUEL INLET (UNMETERED ) FIGURE 6 - THROTTLE & METERING ASSEMBLY MO DAY YEAR MO DAY YEAR 28 of 32
29 THROTTLE LEVER INLET SCREEN FUEL INLET FITTING (UNMETERED ) MIXTURE LEVER FUEL RETURN (TO FUEL PUMP) FUEL OUTLET (METERED ) FIGURE 7 - THROTTLE & CONTROL ASSEMBLY - FRONT VIEW (EXCEPT GTSIO-520-D,F,H,K,L,M,N) IDLE SPEED STOP SCREW CW = INCREASE IDLE MIXTURE ADJUSTMENT CW = ENRICH FIGURE 8 - THROTTLE & CONTROL ASSEMBLY SIDE VIEW (EXCEPT GTSIO-520-D, F, H,, K, L, M, N) MO DAY YEAR MO DAY YEAR 29 of 32
30 INLET SCREEN THROTTLE BODY FUEL CONTROL IDLE SPEED STOP SCREW CW = INCREASE IDLE MIXTURE ADJUSTMENT CCW =ENRICH FIGURE 9 - THROTTLE & CONTROL ASSEMBLY (ALL GTSIO-520 EXCEPT GTSIO-520-C, F & K) LOCK NUT FUEL ADJUSTMENT CW - INCREASE TURBOCHARGER DISCHARGE REFERENCE INLET (UNMETERED ) CENTER PORT (OUTLET) FIGURE 10 - FUEL REGULATOR FOR TURBOCHARGED ENGINES MO DAY YEAR MO DAY YEAR 30 of 32
31 2 FUEL METERED FUEL P.S.I VAPOR VENT RETURN TO FUEL TANK FUEL RETURN FROM FUEL CONTROL FUEL PUMP ASSEMBLY FUEL INLET FROM FUEL TANK MANIFOLD VALVE ASSEMBLY FUEL CONTROL FUEL INJECTORS LOW RELIEF VALVE FUEL SCREEN THROTTLE BODY ADJUSTABLE ORIFICE IDLE MIXTURE ADJUST BYPASS 4 6 DRAIN 2 8 IDLE SPEED STOP SCREW UNMETERED FUEL FUEL P.S.I FIGURE 11 Typical Naturally Aspirated Fuel System Schematic FUEL P.S.I FROM TURBOCHARGER METERED FUEL UPPER DECK THROTTLE AND CONTROL ASSEMBLY UPPER DECK RETURN FUEL FROM FUEL CONTROL FUEL MANIFOLD VALVE ASSEMBLY UPPER DECK FUEL INJECTOR NOZZLE FLOW FLOW FLOW FUEL REGULATOR INLET FUEL FROM ACFT FLOW VAPOR RETURN FLOW FLOW TURBOCHARGER DISCHARGE UPPER DECK METERED FUEL NOZZLE FUEL 10 P.P.H UNMETERED FUEL FUEL PUMP FIGURE 12 Typical Turbo-Charged Fuel System Schematic (With Regulator) FLOW FLOW MO DAY YEAR MO DAY YEAR 31 of 32
32 MO DAY YEAR MO DAY YEAR 32 of 32
33 Signature: Remarks: (Idle RPM mixture rise, magneto drop, etc.) Spec Actual Spec Actual R.P.M. M.A.P. Pressure Altitude - (Set altimeter to Hg) Spec Actual Spec Actual Spec Actual Spec Actual Spec Actual Spec Actual EGT o F TIT o F CHT o F Oil PSI Oil Temp. o F I.A.S. knots Flight Test Data - Record gauge indications o Spec Actual F o F PSI o Spec Actual Spec Actual Spec Actual Spec Actual F CW CCW Fuel Pressure R.P.M. M.A.P. Unmetered Metered EGT TIT Cylinder Head Temp. - o F Adjustment Oil # of turns Fuel System Adjustment - Record engine specifications and actual guage indications. Engine Serial Number: Engine Total Time - New - Overhaul Engine Model: Engine Position: Left Right Front Rear Aircraft Make & Model: Aircraft Registration #: Date: Location: Elevation: OAT: Field Hg:
PURPOSE: To provide magneto to engine timing procedures for all TCM engines.
TELEDYNE CONTINENTAL AIRCRAFT ENGINE MANDATORY SERVICE BULLETIN The Subject Matter Of This Service Bulletin Is Incorporated In Whole Or In Part In An FAA Issued Airworthiness Directive SUBJECT: MAGNETO
More informationSB96-11B FAA APPROVED Supersedes SB96-11A, SB96-11, M84-16
TELEDYNE CONTINENTAL AIRCRAFT ENGINE SERVICE ULLETIN Compliance Will Enhance Safety SUJECT: PROPELLER STRIKES AND HYDRAULIC LOCKS. CATEGORY 3 S96-11 FAA APPROVED Supersedes S96-11A, S96-11, M84-16 PURPOSE:
More informationTurbocharger system components, servicing
21-1 Turbocharger system components, servicing Engine codes: AAZ, 1Z, AHU Observe rules of cleanliness Page 21-10 Turbocharger hoses and lines, connecting Page 21-11 WARNING! Do not re-use any fasteners
More informationRexroth Hydraulic Pump A10VO Series User Manual
Rexroth Hydraulic Pump A10VO Series User Manual Rexroth Hydraulic pump A10VO Series User Manual Revised 5/1/2009 Page 1 of 12 Functional Purpose This pump is preferred over a fixed displacement (gear)
More informationCYLINDER LEAKAGE CHECK (Compression)
TELEDYNE CONTINENTAL AIRCRAFT ENGINE service bulletin M84-15 SUPERSEDES M76-18 Rev.1 Technical Portions are FAA Approved 21 December 1984 TO: SUBJECT: MODELS AFFECTED: Aircraft Manufacturers, Distributors,
More informationTable of Contents. Overview 1. Pump Disassembly 2. Control Disassembly / Reassembly 7. Pump Reassembly 13. Adjustment Procedures DR Control 19
Table of Contents Overview 1 Pump Disassembly 2 Control Disassembly / Reassembly 7 Pump Reassembly 13 Adjustment Procedures DR Control 19 Adjustment Procedures DRG Control 20 Adjustment Procedures DFR
More informationLancair Legacy Annual Condition Inspection Checklist
Lancair Legacy Annual Condition Inspection Checklist Performed by: Completion Date: Complete Maintenance/Inspection Item Comments Pre-Inspection Research AD and Service bulletins Inspect entire airframe
More informationFuel Injection Pump, Rotary (005-014)
Fuel Injection Pump, Rotary View Related Topic Page 1 of 30 Fuel Injection Pump, Rotary (005-014) Table of Contents Summary General Information Preparatory Steps Remove Front Gear Train Rear Gear Train
More informationYour safety and the safety of others are very important.
NATURAL GAS TO PROPANE CONVERSION KIT 090 INSTALLATION INSTRUCTIONS FOR ALTITUDES 0 -,00 FT. ONLY PROPANE CONVERSION KIT SAFETY... INSTALLATION REQUIREMENTS... Tools and Parts... LP Gas Requirements...
More informationP7100 PUMP INSTALLATION INSTRUCTIONS Diesel Care & Performance Inc
P7100 PUMP INSTALLATION INSTRUCTIONS Diesel Care & Performance Inc Installation Timing Pin Location CAUTION: Before installing the injection pump, be sure that number 1 cylinder is at the Top Dead Center
More informationwww.servicechamp.com
1-800-221-0216 Fax: 1-800-472-2281 www.servicechamp.com Service Champ Part 52081 Service Interval every 30,000 miles / Chevrolet 1992-2002 6.5 liter Description and Operation The fuel filter element separates
More informationLYCOMING OPERATOR S MANUAL SECTION 3 OPERATING INSTRUCTIONS
LYCOMING OPERATOR S MANUAL SECTION 3 Page General... 3-1 Prestarting Items of Maintenance... 3-1 Starting Procedures... 3-1 Cold Weather Starting... 3-3 Ground Running and Warm-Up... 3-3 Ground Check...
More informationWHAT YOU DON T KNOW ABOUT ACCUMULATORS CAN KILL YOU!
WHAT YOU DON T KNOW ABOUT ACCUMULATORS CAN KILL YOU! Atlanta (Monroe) GA 770-267-3787 gpm@gpmhydraulic.com www.gpmhydraulic.com What You Don t Know About Hydraulic Accumulators Can Kill You TABLE OF CONTENTS
More informationUniversal Adjustable Fuel Pressure Regulator
Universal Adjustable Fuel Pressure Regulator Installation Instructions for: Part Numbers 25-302 U.S. Patent # 6,298,828! Due WARNING: to the fact that this installation deals with your fuel system this
More informationSystem Saver 318 Air Compressor for Mack E-Tech and ASET Engines
Maintenance Manual 31 System Saver 318 Air Compressor for Mack E-Tech and ASET Engines Revised 08-05 NON-THROUGH DRIVE THROUGH DRIVE Service Notes About This Manual This manual provides service and repair
More informationREMOVAL AND INSTALLATION
303-01C-1 REMOVAL AND INSTALLATION Engine Body On Special Tool(s) Adapter For 303-D043 303-D043-02 or equivalent Special Tool(s) 303-01C-1 Turbocharger Lifting Bracket 303-1266 Wrench, Fan Clutch Nut 303-214
More informationSELF-STEERING AXLE TABLE OF CONTENTS
SELF-STEERING AXLE TABLE OF CONTENTS Section 1 - Introduction Section 2 - Pre-Installation Check List Section 3 - Ride Height Adjustments Section 4 - Suspension Mount Section 5 - Axle Mount Section 6 -
More informationLINDGREN-PITMAN, INC. Super Spool III Installation Instructions
LINDGREN-PITMAN, INC. Super Spool III Installation Instructions LINDGREN-PITMAN, INC. 2615 N.E. 5th Avenue * Pompano Beach, Florida 33064 * U.S.A. (954)943-4243 * (954)943-7877 Fax E-mail: longline@gate.net
More informationFLYBLOCKTIME PA-28-140/160 Aircraft Type Checkout and Currency Quiz. NOTE: There may be one or more correct answers to each question.
FLYBLOCKTIME PA-28-140/160 Aircraft Type Checkout and Currency Quiz Pilot s Name Date NOTE: There may be one or more correct answers to each question. 1 ) The engine in a PA-28-140/160 is a A. Continental
More informationDiesel Fuel Systems. Injection Nozzles
Diesel Fuel Systems Injection Nozzles Unit Terms Injection nozzle Nozzle, nozzle holder, valve, spring assembly Nozzle assembly Valve, body, and spray valve Orifice Small hole Pintle Valve which the end
More informationSELECTION, APPLICATION & MAINTENANCE
DIESEL PROTECTION SYSTEMS TPZ Engine Air Intake Shut Down Valves (Combined Automatic Overspeed and Air Pressure Operated Shut Down Bendix Types) SELECTION, APPLICATION & MAINTENANCE Valve Numbers TPZ-101
More informationMANDATORY SERVICE BULLETIN
652 Oliver Street Williamsport, PA 17701 U.S.A. Tel. +1-800-258-3279 (U.S. and Canada) Tel. +1-570-323-6181 (International) Fax. +1-570-327-7101 www.lycoming.com MANDATORY SERVICE BULLETIN DATE: October
More informationENGINE FUEL FUEL FILTER... FUEL HEATER... INJECTOR... SUPPLY PUMP... COMMON RAIL... FUEL PRESSURE LIMITTER...
FUEL FILTER............................ FUEL HEATER.......................... INJECTOR.............................. SUPPLY PUMP.......................... COMMON RAIL.......................... FUEL PRESSURE
More informationRecharge Procedure for Telemark TVP-2000 and TVP-3500
Recharge Procedure for Telemark TVP-2000 and TVP-3500 Required items: 1.) Refrigeration service manifold. 2.) Charge recovery system. 3.) Dry nitrogen gas. If a high pressure cylinder is used, a pressure
More informationCooling system components, removing and installing
Page 1 of 34 19-1 Cooling system components, removing and installing WARNING! The cooling system is pressurized when the engine is warm. When opening the expansion tank, wear gloves and other appropriate
More informationIndex 11.1. Page. Pumping Systems...11.2-11.4 Intensifiers...11.5 Gas Boosters...11.6-11.7 High Pressure Generators...11.8-11.9
Pumping Systems, Intensifiers, Gas Boosters and High Pressure Generators High Pressure Equipment Company produces a number of components and systems for general industrial, elevated pressure applications.
More informationNot required for most applications Not required for most applications High pressure (12-803 provided) High pressure (12-803 provided)
ELECTRIC FUEL PUMPS P/N 12-801-1, 712-801-1, 12-802-1, 712-802-1, 12-815-1, & 712-815-1 FUEL PRESSURE REGULATORS P/N 12-803, 12-501, 12-804, 12-500, & 15812NOS Installation Instructions THESE INSTRUCTIONS
More informationMustang Series PRESSURE REDUCING CONTROL VALVE WITH PRESSURE SUSTAINING FEATURE. M115-2 (Globe) M1115-2 (Angle) Schematic. Standard Components
Schematic Throttles to reduce high upstream pressure to constant lower downstream pressure Throttles to maintain minimum upstream pressure PRESSURE REDUCING CONTROL VALVE WITH PRESSURE SUSTAINING FEATURE
More informationVolkswagen Jetta, Golf, GTI 1999, 2000 Brake System 47 Brakes - Hydraulic Components (Page GR-47)
47 Brakes - Hydraulic Components (Page GR-47) FS III front brake calipers, servicing Front brake caliper piston, removing and installing FN 3 front brake calipers, servicing Front caliper piston, removing
More informationThe cylinder head bolts tightening stages have been updated as listed in Table 1.
NUMBER: 07 EPA04 MBE 4000-6 S.M. REF.: 1.2.2 ENGINE: MBE 4000 DATE: November 2007 SUBJECT: CYLINDER HEAD BOLTS TIGHTENING STAGES PUBLICATION: 6SE412 The cylinder head bolts tightening stages have been
More informationFloat and Thermostatic Traps Series H, C and X
Hoffman Specialty Installation & Maintenance Instructions HS-(E) and Thermostatic Traps Series H, C and X Series C & NPT Series C NPT Series X NPT Series C NPT Series H Ratings Maximum Max. Operating NPT
More informationInstruction Manual. Please read the manual carefully before installing and using this product. This product is for off road use only.
Instruction Manual Please read the manual carefully before installing and using this product. This product is for off road use only. PARTS 1. LIST BLOW OFF VALVE 1 5. GASKET 1 2. VACUUM HOSE 4.5φ 1 6.
More informationCompressor Service & Maintenance Manual
Compressor Service & Maintenance Manual C Series COMPRESSOR (D)C1103 (D)C1203 (D)C2106 (D)C2206 (D)C3210 Copyright 2006 DCI. All Rights Reserved. 92311, Rev. C, 08/13 1 C1000 Series Service & Maintenance
More informationTech. Services: (800) 477-8326 Fax: (800) 765-8326 Order Entry: (800) 541-1418 Fax: (800) 288-7031 Internet Address: http://www.powerteam.
ORIGINAL INSTRUCTIONS Form No.102842 5 SPX Hydraulic Technologies 5885 11th Street Rockford, IL 61109-3699 USA Tech. Services: (800) 477-8326 Fax: (800) 765-8326 Order Entry: (800) 541-1418 Fax: (800)
More informationPRESSURE REDUCING CONTROL VALVE
Schematics Throttles to reduce high upstream pressure to constant lower downstream pressure Low Flow By-Pass controls at low flows 4 PRESSURE REDUCING CONTROL VALVE with LOW FLOW BY-PASS FEATURE Main Line
More informationPC1131 Electric Air Compressor
Senco Products Inc. 8485 Broadwell Road Cincinnati, Ohio 45244 PC1131 Electric Air Compressor Operating Instructions 2006 by Senco Products, Inc. Warnings for the safe use of this tool are included in
More informationPC1130 Electric Air Compressor
Senco Products Inc. 8485 Broadwell Road Cincinnati, Ohio 45244 PC1130 Electric Air Compressor Operating Instructions 2006 by Senco Products, Inc. Warnings for the safe use of this tool are included in
More informationCDS TROUBLESHOOTING SECTION I. VACUUM. 1.0. Weak vacuum at wand. Gauge reads normal (10hg to 14hg)
CDS TROUBLESHOOTING SECTION I. VACUUM 1.0. Weak vacuum at wand. Gauge reads normal (10hg to 14hg) 1.1. Clogged hoses or wand tube. Disconnect hoses and carefully check for an obstruction. 1.2. Excessive
More informationOregon Fuel Injection
Corporate Office: P.O. Box 21121, VE Pump Removal and Installation Cummins Lock Timed Applications Removal Clean the exterior of the injection pump and mounting surfaces. 1. Disconnect the fuel return
More informationDiagnosing Hydraulic Problems
Diagnosing Hydraulic Problems 1 Problems A pressure test is a key check when you need to determine if a problem is caused by something that is inside or outside of the transmission. Low automatic transmission
More informationINSTALLATION MANUAL MODEL RP-100
INSTALLATION MANUAL FOR 24 VALVE 5.9L CUMMINS POWERED DODGE TRUCKS 2003 THROUGH 2004.5 MODEL RP-100 READ THESE INSTRUCTIONS THOROUGHLY BEFORE BEGINNING INSTALLATION 5400 BUSINESS 50 WEST SUITE 8 573 635-0555
More informationINSTALLATION MANUAL MODEL RP-150
INSTALLATION MANUAL FOR 24 VALVE 5.9L CUMMINS POWERED DODGE TRUCKS 2003 THROUGH 2004.5 MODEL RP-150 READ THESE INSTRUCTIONS THOROUGHLY BEFORE BEGINNING INSTALLATION 5400 BUSINESS 50 WEST SUITE 8 573 635-0555
More informationGPS AutoSteer System Installation Manual
GPS AutoSteer System Installation Manual Supported Vehicles John Deere Combines 9650 STS 9660 STS 9550 CTS 9400 Walker 9600 Walker 9750 STS 9760 STS 9650 CTS 9410 Walker 9610 Walker 9560 STS 9860 STS 9660
More informationSELECTION, APPLICATION AND MAINTENANCE
DIESEL PROTECTION SYSTEMS D-Series Engine Automatic Overspeed Shut Down Valves (Spindle Types with Air Pressure and Manual Shut Down Options) SELECTION, APPLICATION AND MAINTENANCE Valve Numbers D92-AP
More informationSection 7 Adjustment, Repair and Replacement
Section 7 Adjustment, Repair, and Replacement Page 7-1 Section 7 Adjustment, Repair and Replacement Section Contents Page Overview...7-5 Belts Belt Guard Removal/Installation...7-7 Belt Removal/Installation...7-11
More informationMulti Engine Oral Exam Questions
Multi Engine Oral Exam Questions 1. What are the requirements for a multi-engine rating? 2. What is the max rated horse power at sea level? At 12,000 msl? 3. What is the rated engine speed? 4. What is
More informationHow To Fix A Car With A Carbide Engine
Section 12 Adjustment, Repair, and Replacement Page 12-1 Section 12 Adjustment, Repair and Replacement Section Contents Page Overview...12-5 Belts Belt Guard Removal/Installation...12-7 Belt Removal/Installation...12-11
More informationTrouble Shooting Tech Tips Operation
Steering Components TroubleShooting Tech Tips Table of Contents Basic Steering System Operation 2 Sector Shaft Adjustments 4 Drag Link Adjustment 5 Relief Valve/Unloading Valve Adjustment 6 Ross TAS Automatic
More informationFJ2. 2 Ton Trolley Floor Jack Assembly & Operating Instructions
FJ2 2 Ton Trolley Floor Jack Assembly & Operating Instructions READ ALL INSTRUCTIONS AND WARNINGS BEFORE USING THIS PRODUCT. This manual provides important information on proper operation & maintenance.
More informationACCUMULATOR INSTALLATION
7001-7 ACCUMULATOR INSTALLATION BRAKE ACCUMULATORS I 308L93 Rae 7-59710 Issued 6-93 Printed in U.S.A 7001-8 Removal ACCUMULATOR VALVE 1. Park the machine on a level surface and lower the. loader bucket
More informationAdjustment Data MAZDA - 626-2.0 Comprex D - RF-CX
Adjustment Data MAZDA - 626-2.0 Comprex D - RF-CX Engine (general) Engine code RF Capacity 1998 (cc) Idle speed 725 ± 25 Valve clearance Valve clearance Cold Inlet 0.25 (mm) Exhaust 0.35 (mm) Compression
More informationHeating, Ventilation, Air Conditioning and Refrigeration (HVACR)
Heating, Ventilation, Air Conditioning and Refrigeration (HVACR) I. Demonstrate safety skills in typical HVACR work situations to NATE Core Installer Knowledge Areas for Technician Excellence for Safety
More informationINSIDE ENGINE COMPARTMENT TOYOTA AIR CONDITIONING ENGLISH EUROPE,GENERAL,AUSTRALIA
INSIDE ENGINE COMPARTMENT TOYOTA AIR CONDITIONING ENGLISH EUROPE,GENERAL,AUSTRALIA INTRODUCTION IMPORTANT NOTICE This manual has been designed for technicians who are qualified and educated in the proper
More informationSeries 30000 Hose Reels
Operating Instructions and Parts List for Series 30000 Hose Reels - MANUAL DRIVEN - - POWER DRIVEN - SAFETY PRECAUTIONS Personal injury and/or equipment damage may result if proper safety precautions are
More informationFuel System Description. Stromberg 175 CD-2 SE And SU-HS 6 Carburettors
Fuel System Description Stromberg 175 CD-2 SE And SU-HS 6 Carburettors The B 20 A engine is fitted with a horizontal carburettor of typo Stromberg 175 CD-2 SE, see Fig. 60. The B 20 B engine In the l20
More informationInstalling a Probe. Typical Installation
for hazardous locations. Prior to any installation in a Classified Hazardous Location, verify installation methods by the Control Drawing referenced on the product s name tag 2. The Feed Through Assembly
More informationSTANDARD INTEGRATED POWER STEERING
STANDARD INTEGRATED POWER STEERING Mount Pleasant Lane, Lymington, Hampshire SO41 8LS Tel: +44 (0)1590 681445 Fax: +44 (0)1590 681446 www.hypromarine.com Page No. Contents INDEX 1. AMENDMENTS 2. DESCRIPTION
More informationModel 43AP Pneumatic Controller, Style B
Instruction MI 011-476 January 1980 Model 43AP Pneumatic Controller, Style B Installation and Operation Model 43AP Controller continuously detects the difference between a process measurement and its set
More informationFile Number MDRA C20 MANUAL of PROCEDURES for INSPECTION of COMPOSITE AMATEUR-BUILT AIRCRAFT, INSPECTION AND TECHNICAL INFORMATION RECORD
File Number MDRA C20 MANUAL of PROCEDURES for INSPECTION of COMPOSITE AMATEUR-BUILT AIRCRAFT, INSPECTION AND TECHNICAL INFORMATION RECORD GENERAL Section 1.4 FINAL INSPECTION 1. Have all re-inspection
More informationProduct Manual. CVS Type 67AFR Filter Regulator. Introduction. Installation. Description
Product Manual CVS Type 67AFR Filter Regulator Introduction This CVS Controls product manual includes instructions for the installation, adjustment, maintenance and parts ordering of the CVS Type 67AFR
More informationTri-Homo Style Operation and Maintenance Instructions
Tri-Homo Style Operation and Maintenance Instructions One Research Drive Stratford, CT 06615 (203) 375-0063 www.sonicmixing.com 1 Installation and Start-up Do not perform following adjustments without
More informationTRAINING BULLETIN Fire Apparatus Pump Test
TOPIC: TRAINING BULLETIN Fire Apparatus Pump Test EFFECTIVE DATE: 05/06 DOC NO: TB081 CROSS REF: INTRODUCTION District Fire Apparatus Pump Testing is completed on an annual basis. Currently, pump testing
More informationREGULATORS 175/153 Series
175/153 Series 175 HEATING 153 COOLING Watson McDaniel reserves the right to change the designs and/or materials of its products without notice. 2002 Watson McDaniel Company Revised 7/2002 175 / 153 Screwed
More informationAKRON EDUCTORS TROUBLESHOOTING GUIDE OPERATION & THEORY OF EDUCTORS GENERAL OPERATING AND MAINTENANCE INSTRUCTIONS
AKRON EDUCTORS TROUBLESHOOTING GUIDE OPERATION & THEORY OF EDUCTORS GENERAL OPERATING AND MAINTENANCE INSTRUCTIONS Products Include: 60 gpm eductors Style 3060, 3061, 3062 & 3070 95 gpm eductors Style
More informationTECHNICAL BULLETIN. Meritor WABCO Cab Leveling Valves and Chassis Leveling Valves. How the Cab Leveling and Chassis Leveling Valves Work
Revised 02-00 TECHNICAL BULLETIN Meritor WABCO Cab Leveling Valves and Chassis Leveling Valves This technical bulletin covers both cab and chassis leveling valves manufactured by Meritor WABCO. While the
More informationFLUSHOMETER - TANK SYSTEM
Owner s Service Manual 501-A Series FLUSHOMETER - TANK SYSTEM 501-A Series FLUSHMATE 501-A SERIES (D) (E) (C) 2 3 (B) 1 4 (F) (A) 6 5 List of Components for 501-A Series*: 1. Lower Supply Group w/hose
More informationINSTALLATION GUIDE. Your guide to Stromberg 97 carburetor installation and adjustment
INSTALLATION GUIDE If you need further information or assistance, please contact your Genuine Stromberg dealer, or email us direct at tech@stromberg-97.com or log on to our Tech Center at www.stromberg-97.com
More informationAuto-belay Cable Replacement Process
Auto-belay Cable Replacement Process Version 2.00 WARNING: The air pressure in the auto-belay system is what causes the cable to be retracted when releasing the cable or climbing the wall with the cable
More informationSTEERING HANDLEBAR/FRONT WHEEL/ FRONT SHOCK ABSORBER
14 14 STEERING HANDLEBAR/FRONT WHEEL/ SCHEMATIC DRAWING ------------------------------------------------- 14-1 SERVICE INFORMATION------------------------------------------------ 14-2 TROUBLESHOOTING-----------------------------------------------------
More informationPUMP MAINTENANCE SCHEDULE AND CHECKLISTS
PUMP MAINTENANCE SCHEDULE AND CHECKLISTS Providing a maintenance schedule defined specifically by run hours or yardage pumped serves only as a general guideline given the large amount of variables a unit
More information1 5 05-12 5 05-12. Additions, Revisions, or Updates
5 05-12 1 5 05-12 SUBJECT DATE Cylinder Head May 2012 Additions, Revisions, or Updates Publication Number / Title Platform Section Title Change DDC-SVC-MAN-0023 EPA04 MBE 4000 Cylinder Head Additional
More informationEngine. 204-1890 Strobe light, 110V 204-1891 Strobe light, 220V 204-458 Replacement bulb. 204-1057 Compression gauge. 204-166 Dial indicator
The Strobe light checks the unit for: Balance of operating machinery RPM of motors, engine pulleys, fans, etc. Observe belt slippage Strobe light will stop action at speeds from 200 to 6000 RPM 204-1890
More informationSELECTION, APPLICATION AND MAINTENANCE
DIESEL PROTECTION SYSTEMS Automatic Diesel Engine Shut Down System for Safe Area Applications SELECTION, APPLICATION AND MAINTENANCE Series 300 Series 310 SYSTEM DESCRIPTION Suitable for attended engine
More informationVAPOR CYCLE FREON AIR-CONDITIONING CHAPTER 05 - TIME LIMITS/INSPECTIONS LIST OF EFFECTIVE PAGES. List of Effective Pages 1 7 June 2007
CHAPTER 05 - TIME LIMITS/INSPECTIONS LIST OF EFFECTIVE PAGES SECTION PAGE DATE List of Effective Pages 1 7 June 2007 Table of Contents 1-3 05-00-00 601-603 05-11-00 601 and 603 05-11-00 602 7 June 2007
More informationC18 ACERT Fire Pump Tier 3 448 bkw/600 bhp @ 1750 rpm
CATERPILLAR ENGINE SPECIFICATIONS I-6, 4-Stroke-Cycle Diesel Bore...145.0 mm (5.71 in) Stroke...183.0 mm (7.2 in) Displacement... 18.1 L (1,104.53 in3) Aspiration...Turbocharged Aftercooled Compression
More informationHYDRAULIC LIFT TABLE CART 2200-LB.
HYDRAULIC LIFT TABLE CART 2200-LB. OWNER S MANUAL WARNING: Read carefully and understand all MACHINE ADJUSTMENT AND OPERATION INSTRUCTIONS before operating. Failure to follow the safety rules and other
More informationStandard Hydraulic Piping Flushing Procedure
Page 1 of 6 1.0 Scope This procedure covers the minimum technical requirements for cleaning and flushing of Hydraulic and Piping, and related accessories. 2.0 Introduction In hydraulic fluid power systems,
More informationCooling Systems. Table of Contents
Cooling Systems Table of Contents Sub-Headings Safety 2 s 2 Cautions 2 Notes 2 Introduction 2 General Specifications 2 ISB Engine 2 ISC Engine 2 Caterpillar 3126 Engine 2 Types of Coolant 3 ISB Engine
More informationImportant: Please read these instructions carefully and completely before starting the installation. TITAN Fuel Tanks
TITAN pt. no.: 03 0000 0120 Important: Please read these instructions carefully and completely before starting the installation. TITAN Fuel Tanks INSTALLATION INSTRUCTIONS G e n e r a t i o n V Extended
More informationSignature and ISX CM870 Fuel System
Signature and ISX CM870 Fuel System Cummins Ontario Training Center HPI-TP Fuel System Heavy Duty High Pressure Injection - Time Pressure Fuel System The fuel system developed for the Signature and ISX
More informationWynn s Extended Care
Wynn s Extended Care Every car deserves to receive the very best care... especially yours. How Do You Keep Your Reliable Transportation Reliable? Count on Wynn s Because Wynn s has been caring for cars
More informationENGINEERING RELEASE MODEL: LEARJET MODEL 20 AND 35/36 SERIES DRAWING. NO.: 02907011 SHEET: 1 OF 1
ENGINEERING RELEASE DRAWING. NO.: 02907011 MODEL: LEARJET MODEL 20 AND 35/36 SERIES SHEET: 1 OF 1 Butler National Corporation Olathe, Kansas DRAWING TITLE: INSTRUCTIONS FOR CONTINUED AIRWORTHINESS FOR
More informationIntake Manifold: Service and Repair
2000 Chevy Truck S10/T10 P/U 2WD L4-2.2L VIN 4 Copyright 2008, ALLDATA 9.90 Page 1 Intake Manifold: Service and Repair Removal Procedure 1. Disconnect the battery negative cable. Refer to Battery Replacement.
More informationApproval of this procedure is provided by signatory indicated in the approval block at the footer of Page #1, for and on behalf of Jabiru Pty. Ltd.
Jabiru Service Bulletin Number A3 Fuel System Cleaning Note on Revision 2. Revision 2 of this Service Bulletin updates the cleaning procedure using knowledge that has been gained by Jabiru. This revision
More informationCat Electronic Technician 2015A v1.0 Product Status Report 4/20/2016 2:49 PM
Page 1 of 19 Cat Electronic Technician 2015A v1.0 Product Status Report 2:49 PM Product Status Report Parameter Value Product ID WRK00337 Equipment ID WRK00337 Comments A01-52 C9 330D (THX37891) Parameter
More informationNITROUS TRANSFER PUMP INSTRUCTIONS
NITROUS TRANSFER PUMP INSTRUCTIONS SAFETY TIPS Never directly inhale nitrous oxide. When inhaled in large quantities, nitrous oxide can cause respiratory ailments or in extreme cases, death by suffocation.
More informationENGINE COOLING SYSTEM
ENGINE COOLING SYSTEM 1988 Toyota Celica 1987-88 TOYOTA Engine Cooling Systems Celica DESCRIPTION The basic liquid cooling system consists of a radiator, water pump, thermostat, cooling fan, pressure cap,
More informationPVH131/141 Variable Displacement Piston Pump - 11 Design
Service Data Vickers Piston Pumps PVH131/141 Variable Displacement Piston Pump - 11 Design Revised 05/01/97 M-2209-S Maximum Adjustable Stop S Option 913341 Locknut Torque 25-50 N.m. (18-37 lb. ft.) Torque
More informationFlow Control Valves. Note: Also see R04C3 on page DC1. Denotes New Winner s Circle Product Line. Catalog HY15-3502/US
Catalog HY15-352/US Contents Control SERIES CAVITY DESCRIPTION FLOW PRESSURE PAGE NO. LPM/GPM BAR/PSI NEED VALVES J2A2... C8-2... Needle Valve, Cartridge Type...45/12... 42/6... 5-6 NVH81... C8-2... Needle
More informationWIKA INSTRUMENT CORPORATION
WIKA INSTRUMENT CORPORATION Instruction Manual GAUGE PRESSURE INDICATOR Series 1500 Series 1000 Series 300 WIKA Instrument Corporation 1000 Wiegand Boulevard Lawrenceville, GA 30043 1-888-945-2872 http://www.wika.com
More informationTITAN Fuel Tanks. INSTALLATION INSTRUCTIONS G e n e r a t i o n V
TITAN pt. no.: 02 0000 0143 Important: Please read these instructions carefully and completely before starting the installation. TITAN Fuel Tanks INSTALLATION INSTRUCTIONS G e n e r a t i o n V Extended
More informationPOSEIDON 2-29, 2-25 & 2-22 POSEIDON 2-29, 2-25 & 2-22 XT
POSEION 2-29, 2-25 & 2-22 POSEION 2-29, 2-25 & 2-22 XT Repair Manual Index A. Safety precautions 3 B. Technical data 4 C. Structure 5-6. Service / Repair 7-23 E. Tools 24 F. Function 25-26 G. Electric
More informationAIRCRAFT PERFORMANCE Pressure Altitude And Density Altitude
Performance- Page 67 AIRCRAFT PERFORMANCE Pressure Altitude And Density Altitude Pressure altitude is indicated altitude corrected for nonstandard pressure. It is determined by setting 29.92 in the altimeter
More informationFLOWMETER INSTALLATION INSTRUCTIONS
SAFETY FIRST: Follow ALL safety precautions when working on motor equipment-wear safety glasses! Fuel vapors and liquid are extremely flammable and explosive, personal injury and/or property damage could
More informationMODEL G300 BRAKE BLEEDER
MODEL G300 BRAKE BLEEDER Installation, Operation & Repair Parts Information Branick Industries, Inc. 4245 Main Avenue P.O. Box 1937 Fargo, North Dakota 58103 REV060616 P/N: 81-0035G 1 THIS PAGE INTENTIONALLY
More informationDavcron Concrete Agitator - Operations Manual
Davcron Concrete Agitator - Operations Manual THE DAVCRON AGITATOR MUST BE OPERATED BY TRAINED AND AUTHORISED PERSONNEL ONLY DAVCRON ENGINEERING PTY LTD General Engineering & Maintenance Contractors -
More information300 Series PA Pump and Cooler Assemblies
Type 300 Series PA Sizes 300 thru 370 (Page 1 of 9) 300 Series PA Pump and Cooler Assemblies Pump and Cooler Assemblies with Air/Oil Heat Exchanger When compact gear drives require assistance to dissipate
More information15GAL STEEL OIL DRAIN WITH 110V PUMP
15GAL STEEL OIL DRAIN WITH 110V PUMP OWNER S MANUAL WARNING: Read carefully and understand all ASSEMBLY AND OPERATION INSTRUCTIONS before operating. Failure to follow the safety rules and other basic safety
More informationFailure to comply with the following cautions and warnings could cause equipment damage and personal injury.
1.0 IMPORTANT RECEIVING INSTRUCTIONS Visually inspect all components for shipping damage. Shipping Damage is not covered by warranty. If shipping damage is found, notify carrier at once. The carrier is
More informationClass 5 to 7 Truck and Bus Hydraulic Brake System
Class 5 to 7 Truck and Bus Hydraulic Brake System Diagnostic Guide 1st Edition * 5+0 Important Service tes The information in this publication was current at the time of printing. The information presented
More information